Robust gain scheduled control of a space launcher by introducing LQG/LTR ideas in the NCF robust stabilisation problem

Mohamed Abbas-Turki, Gilles Duc, Benoît Clement, Spilios Theodoulis

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

5 Citations (Scopus)

Abstract

A space launcher is a time-varying plant which is known to be hard to control, due to time and frequency-domain constraints and parameters uncertainties. In this paper, this problem is solved by interpolating LTI controllers designed for different instants of the flight. Such controllers are obtained by combining the NCF robust control problem with the LQG/LTR approach, the later being useful to design the compensators included in the first one.

Original languageEnglish
Title of host publicationProceedings of the 46th IEEE Conference on Decision and Control 2007, CDC
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages2393-2398
Number of pages6
ISBN (Print)1424414989, 9781424414987
DOIs
Publication statusPublished - Dec 2007
Externally publishedYes
Event46th IEEE Conference on Decision and Control 2007, CDC - New Orleans, LA, United States
Duration: 12 Dec 200714 Dec 2007

Publication series

NameProceedings of the IEEE Conference on Decision and Control
ISSN (Print)0743-1546
ISSN (Electronic)2576-2370

Conference

Conference46th IEEE Conference on Decision and Control 2007, CDC
Country/TerritoryUnited States
CityNew Orleans, LA
Period12/12/0714/12/07

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